• Title/Summary/Keyword: 충돌 임계 속도

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A Study on the Behavior of Droplets Colliding with Parallel Wires (평행 와이어와 충돌하는 액적 거동에 관한 연구)

  • Na, J.K.;Noh, D.H.;Jung, Y.J.;Kang, B.S.
    • Journal of ILASS-Korea
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    • v.26 no.3
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    • pp.149-156
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    • 2021
  • In this study, the behavior of the droplet colliding with parallel wires was analyzed by time-delay photography. The impact behavior modes and the critical capture speed were analyzed by changing fluids, the droplet velocity, the wire diameter and the distance between wires. Seven typical modes of impacting droplet on parallel wires were observed. The tendency of mode change was generally similar when the wire diameter was changed, but the increase of the wire diameter caused the increase of the droplet velocity at which the mode changed. The modes at the highest droplet velocity were the splitting mode when the wires were closest, the passing and splitting mode in the middle, and the passing mode when the wires were farthest apart. The critical capture speed increased as the wire diameter increased and the distance between wires decreased. The ethanol droplet showed the lowest critical capture speed.

A Numerical Study on the Shock Resistance Test of Aluminium 2519 Plate (알루미늄 2519 판재의 충격저항성 평가에 대한 수치 해석적 연구)

  • Koo Man-Hoi;Woo Ho-Gil
    • Journal of the Korea Institute of Military Science and Technology
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    • v.7 no.3 s.18
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    • pp.11-20
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    • 2004
  • In this paper, the acceptance criteria(Striking Velocities) for the A12519 weldments have been developed. Dynamic impact simulation of A12519 plate was achieved by using LS-DYNA, and predict the projectile velocity and the crack length. Also, Ballistic impact tests of A12519 plate have been performed, and compared with analysis results. Critical velocities of A12519 plate were acquired respectively, and striking velocities of A12519 weldments were calculated. Present work data will be used by basic data in ballistic impact test for A12519 weldments.

Whiplash Injury Conditions of Rear-End Collisions at Low-Speed (저속 추돌사고에서 목 상해 조건에 대한 연구)

  • Kim, Myeongju;Yun, Ilsoo
    • The Journal of The Korea Institute of Intelligent Transport Systems
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    • v.18 no.2
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    • pp.58-76
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    • 2019
  • As the number of reported injuries has tended to increase over time, large hospitalization expenditure from excessive medical treatments and hospitalization, and insurance frauds associated with moral hazard in minor collisions have caused a global societal problem. Many occupants of rear-ended vehicles involved in rear-end collisions complain of whiplash injury, which is also known as neck injury, without any anatomical and radiological evidence. With only clinical symptoms, stating that a whiplash injury is a type of injury defined by the Abbreviated Injury Scale would be difficult. Therefore, this study focuses on minor rear-end collisions, where the rear-ender vehicle collides with the rear-ended vehicle at rest. The mathematics dynamic model is employed to simulate a total of 100 rear-end collision scenarios based on various weights and collision speeds and identify how the weights and speeds of both vehicles influence the risk of whiplash injury in occupants involved in minor rear-end collisions. The possibility of an injury is very high when the same-weight vehicles are involved in accidents at collision speeds of 15 km/h or higher. The possibilities are 36% and 84% with collision speeds of 15 km/h and 20 km/h, respectively, if weights are disregarded.

Structural Behavior Evaluation of a Cable-Stayed Bridge Subjected to Aircraft Impact: A Numerical Study (항공기 충돌에 대한 사장교의 구조거동 평가: 수치해석적 접근)

  • Choi, Keunki;Lee, Jungwhee;Chung, Chul-Hun;An, Dongwoo;Yoon, Jaeyong
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.34 no.3
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    • pp.137-149
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    • 2021
  • Cable-stayed bridges are infrastructure facilities of a highly public nature; therefore, it is essential to ensure operational safety and prompt response in the event of a collapse or damage caused by natural and social disasters. Among social disasters, impact accidents can occur in bridges when a vehicle collides with a pier or when crashes occur due to aircraft defects. In the case of offshore bridges, ship collisions will occur at the bottom of the pylon. In this research, a procedure to evaluate the structural behavior of a cable-stayed bridge for aircraft impact is suggested based on a numerical analysis approach, and the feasibility of the procedure is demonstrated by performing an example assessment. The suggested procedure includes 1) setting up suitable aircraft impact hazard scenarios, 2) structural modeling considering the complex behavior mechanisms of cable-stayed bridges, and 3) structural behavior evaluation of cable-stayed bridges using numerical impact simulation. It was observed that the scenario set in this study did not significantly affect the target bridge. However, if impact analysis is performed through various scenarios in the future, the load position and critical load level to cause serious damage to the bridge could be identified. The scenario-based assessment process employed in this study is expected to facilitate the evaluation of bridge structures under aircraft impact in both existing bridges and future designs.

A Study on Restrictions on Entry of Drones into No-Flight Zones using Self-Drop (Self-Drop을 이용한 드론의 비행 금지구역 진입 제한에 관한 연구)

  • Jang-Won, Kim
    • The Journal of Korea Institute of Information, Electronics, and Communication Technology
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    • v.15 no.6
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    • pp.457-462
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    • 2022
  • Recently, a variety of cultural life using drones as an entertainment tool has been created, and in order to realize this, more and more users are using drones with good performance enough to invade the no-flight zone. Drones for satisfying entertainment activities must have long flight times and be able to fly long distances, which can often cause great damage by invading no-flight zones or causing unwanted flight crashes. In this study, in order to solve this problem, a no-flight zone is set with GCS(Ground Control System), and when flying at a critical speed of 10km/h or less, the drone is safely operated by not entering the critical distance 10m away from the no-flight zone, and the critical speed A method was proposed to prevent the drone from entering the no-flight zone by allowing the drone to self-drop by GCS control when it flies beyond the threshold and enters the critical distance. As a result of a total of 44 repeated experiments in a specific experimental area with the proposed method, the drone safely self-dropped except for the case where it crossed the restricted area once or twice. It was found to be an appropriate way to prevent this.

Structure Analysis of Ship′s Collision Causes using Fuzzy Structural Modeling (퍼지구조모델을 이용한 선박충돌사고 원인의 구조분석)

  • Yang, Won-Jae
    • Journal of Navigation and Port Research
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    • v.27 no.2
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    • pp.137-143
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    • 2003
  • The prevention of marine accidents has been a important topic in marine society for long time, and various safety policies and countermeasures have been developed and applied to prevent those accidents. In spite of these efforts, however, significant marine accidents have taken place intermittently. Ship is being operated under a highly dynamic environments, and many factors are related with ship's collision, whose factors are interacting. So, the analysis on ship's collision causes are very important to prepare countermeasures which will ensure the safe navigation. This study analysed the ship's collision data over the past 10 years(1991-2000), which is compiled by Korea Marine Accidents Inquiry Agency. The analysis confirmed that‘ship's collision’is occurred most frequently and the cause is closely related with human factor. The main purpose of this study is to analyse human factor. For this, the structure of human factor is analysed by the questionnaire methodology. Marine experts were surveyed based on major elements that were extracted from the human factor affecting to ship's collision. FSM has been widely adopted in modeling a dynamic system which is composed of human factors. Then, the structure analysis on the causes of ship's collision using FSM are performed. This structure model could be used in understanding and verifying the procedure of real ship's collision. Furthermore it could be used as the model to prevent ship's collision and reduce marine accidents.

A Study on the Possibility of Damage by Anti-aircraft Debris between the Response of Unmanned Aircraft (무인기 대응 간 대공무기 파편에 의한 피해 가능성 연구)

  • Kim, Sea Ill;Shin, Jin
    • Journal of the Korea Society for Simulation
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    • v.29 no.3
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    • pp.1-8
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    • 2020
  • When enemy drones infiltrate large urban areas, various forms of great republics are deployed in large areas to respond. Due to the characteristics of a large number of government-run aircraft, the residual coal, other than the hit bullet, falls into various sizes of debris after its own explosion. The damage rate was analyzed by dividing the debris into anti-aircraft guns and guided weapons by deriving four factors: critical speed, fragmentation mass, initial speed of debris, and object collision speed, which can cause damage to human life as the debris falls to the ground. In the future, the North is expected to infiltrate the capital city of Seoul by operating unmanned aerial vehicles, which are asymmetric forces, and the damage could be minimized by setting up pre-fatal and fire-restricted zones to minimize casualties between responses.

The Vehicle Accident Reconstruction using Skid and Yaw Marks (스키드마크 및 요마크를 이용한 차량사고재구성)

  • 이승종;하정섭
    • Journal of the Korean Society for Precision Engineering
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    • v.20 no.12
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    • pp.55-63
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    • 2003
  • The traffic accident is the prerequisite of the traffic accident reconstruction. In this study, the traffic accident (forward collision) and traffic accident reconstruction (inverse collision) simulations are conducted to improve the quality and accuracy of the traffic accident reconstruction. The vehicle and tire models are used to simulate the trajectories for the post-impact motion of the vehicles after collision. The impact dynamic model applicable to the forward and inverse collision simulations is also provided. The accuracy of impact analysis for the vehicular collision depends on the accuracy of the coefficients of restitution and friction. The neural network is used to estimate these coefficients. The forward and inverse collision simulations for the multi-collisions are conducted. The new method fur the accident reconstruction is proposed to calculate the pre-impact velocities of the vehicles without using the trial and error process which requires the repeated calculations of the initial velocities until the forward collision simulation satisfies with the accident evidences. This method estimates the pre-impact velocities of the vehicles by analyzing the trajectories of the vehicles. The vehicle slides on a road surface not only under the skidding during an emergency braking but also under the steering. A vehicle over steering or cornering with excessive speed loses the traction and leaves tile yaw marks on the road surface. The new critical speed formula based on the vehicle dynamics is proposed to analyze the yaw marks and shows smaller errors than ones of the existing critical speed formula.

반도체 및 디스플레이 세정 공정용 $CO_2$ 클러스터 장비의 클러스터 발생 특성 분석

  • Choe, Hu-Mi;Jo, Yu-Jin;Lee, Jong-U;Kim, Tae-Seong
    • Proceedings of the Korean Vacuum Society Conference
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    • 2013.02a
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    • pp.303-303
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    • 2013
  • 표면에 부착된 나노/마이크로 입자는 다양한 분야에서 오염물질로 작용한다. 특히 형상이 미세하고 공정 단계가 복잡한 반도체 및 디스플레이 등의 전자 소자 공정에서 미치는 영향이 크다. 따라서 입자상 오염물질의 제거에 관하여 상용화된 습식 세정 방법이 다양하게 존재하지만 표면 손상, 화학 반응, 부산물, 세정 효율 등 여러 가지 문제점이 있어 새로운 세정 방법이 요구된다. 이에 건식 세정 방법, 그 중에서도 입자의 충돌을 통해 제거하는 방법인 에어로졸 세정, 필렛 세정 등이 개발되었으나 마이크로 크기로 생성되는 입자로 인하여 형상의 손상이 크다. 따라서 본 연구에서는 나노 단위로 기체/고체 혼합물만 생성하여 세정하는 가스 클러스터 세정 방법을 이용하여 이러한 문제점을 해결하고자 하였다. 클러스터 세정 장비를 이용한 표면 처리는 충돌에 의한 제거에 기반한다. 따라서 생성 및 가속되는 클러스터로부터 대상으로 전달되는 운동량의 정도가 세정 특성에 영향을 미치며 이는 생성되는 클러스터의 크기에 종속적이다. 생성 클러스터의 크기 분포는 분사 거리, 유량, 분사 각도, 노즐 냉각 온도 등의 변수에 관한 함수이다. 따라서 본 연구에서는 $CO_2$ 클러스터를 이용한 세정 특성을 정의 및 제어하기 위하여 생성되는 클러스터 특성에 관하여 이론적, 수치 해석적, 실험적 연구를 수행하였다. 먼저, $CO_2$의 물리적 특성 및 이를 이용한 특정 크기 오염 물질을 제거하는데 요구되는 임계 클러스터 크기 계산을 이론적으로 구하였다. 이는 오염물질의 부착력과 클러스터의 운동량 전달에 의한 제거력의 비교를 통해 이루어졌다. 두 번째로 클러스터 크기분포를 수치 해석적으로 예측하기 위하여 각 조건에 대하여 유동해석을 수행하고 이를 통해 구해진 노즐 내 기체의 냉각 속도를 GDE (General Dynamic Equation) 계산에 대입하여 구하였다. 마지막으로 PBMS(Particle Beam Mass Spectrometer)를 이용하여 실험적으로 클러스터 크기분포를 각 조건에 대하여 구할 수 있었다. 또한 크기 분포 경향에 대한 간접적 확인을 위하여 포토레지스트가 코팅된 웨이퍼에 클러스터의 충격으로 생성된 크레이터 크기의 경향을 분석하였다. 이와 같은 방법에 의하여 생성되는 클러스터는 노즐의 유량 증가, 온도 상승에 각각 비례하여 작아지는 것을 확인할 수 있었다.

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Peducing the Overhead of Virtual Address Translation Process (가상주소 변환 과정에 대한 부담의 줄임)

  • U, Jong-Jeong
    • The Transactions of the Korea Information Processing Society
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    • v.3 no.1
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    • pp.118-126
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    • 1996
  • Memory hierarchy is a useful mechanism for improving the memory access speed and making the program space larger by layering the memories and separating program spaces from memory spaces. However, it needs at least two memory accesses for each data reference : a TLB(Translation Lookaside Buffer) access for the address translation and a data cache access for the desired data. If the cache size increases to the multiplication of page size and the cache associativity, it is difficult to access the TLB with the cache in parallel, thereby making longer the critical timing path in the processor. To achieve such parallel accesses, we present the hybrid mapped TLB which combines a direct mapped TLB with a very small fully-associative mapped TLB. The former can reduce the TLB access time. while the latter removes the conflict misses from the former. The trace-driven simulation shows that under given workloads the proposed TLB is effective even when a fully-associative mapped TLB with only four entries is added because the effects of its increased misses are offset by its speed benefits.

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